发明名称 |
BYPASS TURBOJET ENGINE NACELLE |
摘要 |
The nacelle (1) comprises an air intake (5) upstream of the turbojet engine (2), a middle section (6) an internal casing (6a) of which is intended to surround a fan (3) of the turbojet engine (2), and a downstream section (7) comprising an external structure (7a)which is rigidly connected to a downstream part of the casing (6a) of the fan (3) so as to support the turbojet engine (2) and has means of attachment to a strut (12) intended to be connected to a fixed structure (13) of an aeroplane.
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申请公布号 |
US2010040466(A1) |
申请公布日期 |
2010.02.18 |
申请号 |
US20070445421 |
申请日期 |
2007.10.05 |
申请人 |
AIRCELLE |
发明人 |
VAUCHEL GUY BERNARD;COLLIER JEROME;DHAINAULT PATRICE;CONTE FRANCOIS;HILLEREAU NICOLAS;CHOUARD PIERRE-ALAIN;LEFORT GUILLAUME |
分类号 |
F01D25/28;F02K3/02;F16M13/00 |
主分类号 |
F01D25/28 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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